Airfoil Tools
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Airfoil database search

Search the 1638 airfoils available in the databases filtering by name, thickness and camber. Click on an airfoil image to display a larger preview picture. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of Reynolds numbers.

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(goe462-il) GOE 462 AIRFOIL

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GOE 462 AIRFOILGottingen 462 airfoil
Max thickness 11% at 9.9% chord
Max camber 13.4% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe464-il) GOE 464 AIRFOIL

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GOE 464 AIRFOILGottingen 464 airfoil
Max thickness 7.7% at 7.4% chord
Max camber 9.9% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe474-il) GOE 474 AIRFOIL

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GOE 474 AIRFOILGottingen 474 airfoil
Max thickness 7% at 30% chord
Max camber 2.9% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe476-il) GOE 476 AIRFOIL

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GOE 476 AIRFOILGottingen 476 airfoil
Max thickness 14.5% at 29.5% chord
Max camber 5.2% at 39.5% chord
Source UIUC Airfoil Coordinates Database

(goe477-il) GOE 477 AIRFOIL

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GOE 477 AIRFOILGottingen 477 airfoil
Max thickness 10.1% at 30% chord
Max camber 4.9% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe478-il) GOE 478 AIRFOIL

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GOE 478 AIRFOILGottingen 478 airfoil
Max thickness 13.4% at 29.6% chord
Max camber 4.3% at 39.6% chord
Source UIUC Airfoil Coordinates Database

(goe479-il) GOE 479 AIRFOIL

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GOE 479 AIRFOILGottingen 479 airfoil
Max thickness 11.6% at 30% chord
Max camber 4% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe480-il) GOE 480 AIRFOIL

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GOE 480 AIRFOILGottingen 480 airfoil
Max thickness 11.8% at 30% chord
Max camber 5.5% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe481-il) GOE 481 AIRFOIL

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GOE 481 AIRFOILGottingen 481 airfoil
Max thickness 13.4% at 9.6% chord
Max camber 8.8% at 39.4% chord
Source UIUC Airfoil Coordinates Database

(goe481a-il) GOE 481A AIRFOIL

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GOE 481A AIRFOILGottingen 481A airfoil
Max thickness 15.3% at 29.4% chord
Max camber 5.5% at 39.4% chord
Source UIUC Airfoil Coordinates Database
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